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MR-512
Part of MR-500 engine series Family
MR-512
MR-512
Credit: Aerojet Redmond
Redmond Hydrazine rocket engine. In Production. Low-voltage bus arcjet system. Input power 1780 W at 35 V DC.

Status: In Production. Thrust: 0.25 N (0.06 lbf). Unfuelled mass: 7.23 kg (15.93 lb). Specific impulse: 502 s. Burn time: 3,780,000 s. Height: 0.25 m (0.82 ft). Diameter: 0.0430 m (0.1410 ft).

Engine: 7.23 kg (15.93 lb). Restarts: 1170.



Family: Storable liquid. Country: USA. Agency: Redmond.

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